SBLI control for wings and inlets

Author:

Babinsky Holger,Ogawa Hideaki

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Reference27 articles.

1. Pearcey, H.H.: Shock-induced separation and its prevention by design and boundary layer control. In: Boundary Layer and Flow Control, vol. 2, pp 1166–1344. Pergamon Press, (1961)

2. Mitchell, G.A., Davis, R.W.: Performance of centerbody vortex generators in an axisymmetric mixed-compression inlet at mach numbers from 2.0 to 3.0, NASA TN D-4675 (1968)

3. Neumann, H.E., Wasserbauer, J.F., Shaw, R.J.: Performance of vortex generators in a Mach 2.5 low-bleed Full-scale 45-percent-internal-contraction axisymmetric inlet, NASA TM X-3195 (1975)

4. Reichert B.A. and Wendt B.J. (1996). Improving curved subsonic diffuser performance with vortex generators. AIAA J. 34(1): 65–72

5. Doerffer, P., Szwaba, R.: Shock wave-boundary layer interaction control by streamwise vortices, In: Proceedings of the 21st International Congress of Theoretical and Applied Mechanics. Springer Warsaw, Poland, (2005)

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